CN214603326U

CN214603326U - Aeroengine part processing equipment

Info

Publication number: CN214603326U
Application number: CN202120307665.2U
Authority: CN
Inventors: 吴江; 赵严; 吴勇生; 赵玉琼
Original assignee: Jiangsu Jianghangzhi Aircraft Engine Components Research Institution Co Ltd
Current assignee: Jiangsu Jianghangzhi Aircraft Engine Components Research Institution Co Ltd
Priority date: 2021-02-03
Filing date: 2021-02-03
Publication date: 2021-11-05
Anticipated expiration: 2031-02-03

Abstract

The utility model belongs to the technical field of aero-engine production and processing, in particular to an aero-engine component processing device, which comprises a U-shaped processing table, wherein a cylinder is arranged on the upper end surface of the U-shaped processing table, an installation frame is arranged on the lower end surface of a connecting rod, a motor is arranged at the inner bottom end of the installation frame, a processing tool is arranged on the lower end surface of a rotating shaft, a placing table is fixedly connected with the inner bottom end of the U-shaped processing table, two dust collection boxes are fixedly connected with the inner bottom end of the U-shaped processing table, the upper end surfaces of the two dust collection boxes are both communicated with a dust inlet pipe, two dust collection fans are arranged on the outer side wall of the dust inlet pipe, and a dust collection head is arranged at the opposite end of the two dust inlet pipes, thereby achieving the effect of conveniently sucking and collecting dust and debris generated by processing in the process of engine components and conveniently keeping the processing device clean, the problem that dust generated by long-term suction and processing of workers damages the health of the workers is avoided.

Description

Aeroengine part processing equipment

Technical Field

The utility model relates to an aeroengine production and processing technology field, concretely relates to aeroengine part processing equipment.

Background

An aero-engine (aero-engine) is an engine for providing power required by flying of an aircraft, is a highly complex and precise thermal machine, is known as 'industrial flower' as the heart of the aircraft, directly influences the performance, reliability and economy of the aircraft, and is an important body of national science and technology, industry and national defense strength.

The existing aeroengine part processing equipment is inconvenient for absorbing and collecting dust and fragments generated by processing in the processing process of engine parts, and needs workers to clean the dust and the fragments manually at regular intervals, and meanwhile, the workers easily damage the health of the bodies by absorbing the dust generated by processing for a long time.

SUMMERY OF THE UTILITY MODEL

For solving the problem that provides in the above-mentioned background art, the utility model provides an aeroengine part processing equipment has the dust and the piece that produce to processing conveniently in the engine part course of working and absorbs and collect the processing to conveniently make this processing equipment keep clean, avoid the staff to inhale the characteristics of the dust harm healthy problem that processing produced for a long time.

In order to achieve the above object, the utility model provides a following technical scheme: an aircraft engine part processing device comprises a U-shaped processing table, wherein an air cylinder is installed on the upper end face of the U-shaped processing table, the output end of the air cylinder is detachably connected with a connecting rod, the lower end of the connecting rod penetrates through the U-shaped processing table and extends into the U-shaped processing table, an installation frame is installed on the lower end face of the connecting rod, a motor is installed at the bottom end inside the installation frame, the output end of the motor is detachably connected with a rotating shaft, the lower end of the rotating shaft penetrates through the installation frame and extends to the lower side of the installation frame, a processing tool is installed on the lower end face of the rotating shaft, a placing table is fixedly connected with the bottom end inside the U-shaped processing table, two dust collection boxes are fixedly connected with the bottom end inside the U-shaped processing table and are respectively located on the left side and the right side of the placing table, dust inlet pipes are communicated with the upper end faces of the two dust collection boxes, and dust collection fans are installed on the outer side walls of the two dust inlet pipes, and dust suction heads are arranged at the opposite ends of the two dust inlet pipes.

In order to add man-hour to engine part and make things convenient for to be located to place bench end and fix engine part, avoid engine part aversion in the course of working to cause the problem of processing failure, conduct the utility model relates to an aeroengine part processing equipment is preferred, two risers of the inside bottom fixedly connected with of U type processing platform, two the riser is mutually carried on the back in the body one end respectively with two relative one end fixed connection of dust collecting box, two automatically controlled telescopic link, two are all installed to the relative one end of riser arc clamp splice, two are all installed to the relative one end of automatically controlled telescopic link the lower terminal surface of arc clamp splice all with the up end parallel and level of placing the platform.

Dust and piece to taking out collection in the box are handled in order to make things convenient for the utility model relates to an aeroengine part processing equipment is preferred, two the preceding terminal surface of dust collecting box all can be dismantled and be connected with and take out the box, two take out the preceding terminal surface of box and all install the handle.

In order to avoid two arc clamp splices to treat the problem that the engine part outer wall of processing caused the damage, conduct the utility model relates to an aeroengine part processing equipment is preferred, two the equal fixedly connected with rubber pad of inside wall of arc clamp splice.

Treat the engine part of processing and place the coefficient of friction between the platform in order to increase, avoid treating the engine part of processing and place the easy gliding problem that takes place when placing the bench end, conduct the utility model relates to an aeroengine part processing equipment is preferred, place the up end fixedly connected with antiskid line of platform.

In order to improve the stability when this equipment is placed ground, as the utility model relates to an aeroengine part processing equipment is preferred, four evenly distributed's sucking disc stabilizer blade are installed to the lower terminal surface of U type processing platform.

In order to control the operation and the closing of this equipment conveniently, as the utility model relates to an aeroengine part processing equipment is preferred, control panel is installed to the preceding terminal surface of U type processing platform.

Compared with the prior art, the beneficial effects of the utility model are that:

1. the aeroengine part processing equipment is used for placing an engine part to be processed at the upper end of a placing table during processing, then the cylinder is started, the connecting rod drives the processing tool to move to a corresponding position, the motor is started, the rotating shaft rotates to drive the processing tool to process the engine part, dust and debris are easily generated in the processing process, workers easily damage the health after inhaling for a long time, then the two dust absorption fans are started during processing, dust and debris generated during processing enter the dust inlet pipe through the dust absorption head and are conveyed into the dust collection box, thereby achieving the effect of conveniently absorbing, collecting and treating the dust and the scraps generated in the processing process of the engine parts, and conveniently make this processing equipment keep clean, avoid the staff to inhale the problem that the dust that processing produced harmd healthy for a long time.

2. This kind of aeroengine part processing equipment, to treat the engine part of processing place the bench end after, open two automatically controlled telescopic links, drive two arc clamp splice with the engine part clamp tightly fix to placing the bench end to reached engine part man-hour convenient to be located to place the bench end and carry out the effect fixed to engine part, avoided engine part aversion to cause the problem of processing failure in the course of working.

3. This kind of aeroengine part processing equipment, when handling the processing dust and the piece of collection, hold the handle, will take out the box and take out from dust collecting box the place ahead, handles dust and the piece of taking out the box collection to reached and conveniently handled dust and the piece of taking out the box in the collection.

In conclusion, this kind of aeroengine part processing equipment has the dust and the piece that conveniently produce processing in to engine part course of working and absorbs and collect the processing to conveniently make this processing equipment keep clean, avoid the staff to inhale the characteristics of the dust harm healthy problem that the processing produced for a long time.

Drawings

The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:

FIG. 1 is a front view of an aircraft engine component machining apparatus of the present invention;

FIG. 2 is a cross-sectional view of an aircraft engine component processing apparatus of the present invention;

FIG. 3 is a structural view of the arc-shaped clamping block of the present invention;

fig. 4 is a structural view of the placing table of the present invention.

In the figure, 1, a U-shaped processing table; 101. a sucker support leg; 2. a cylinder; 201. a connecting rod; 202. installing a frame; 203. a motor; 204. a rotating shaft; 205. a processing tool; 3. a placing table; 301. a vertical plate; 302. an electric control telescopic rod; 303. an arc-shaped clamping block; 304. a rubber pad; 305. anti-skid lines; 4. a dust collection box; 401. a dust inlet pipe; 402. a dust collection fan; 403. a dust collection head; 404. drawing the box; 405. a handle; 5. a control panel.

Detailed Description

In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.

In the description of the present invention, it is to be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on those shown in the drawings, and are merely for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention. In addition, in the description of the present invention, "a plurality" means two or more unless specifically limited otherwise.

Referring to fig. 1-3, the present invention provides the following technical solutions: an aircraft engine component processing device comprises a U-shaped processing table 1, wherein an air cylinder 2 is installed on the upper end face of the U-shaped processing table 1, the output end of the air cylinder 2 is detachably connected with a connecting rod 201, the lower end of the connecting rod 201 penetrates through the U-shaped processing table 1 and extends to the inside of the U-shaped processing table 1, the lower end face of the connecting rod 201 is provided with a mounting frame 202, the inner bottom end of the mounting frame 202 is provided with a motor 203, the output end of the motor 203 is detachably connected with a rotating shaft 204, the lower end of the rotating shaft 204 penetrates through the mounting frame 202 and extends to the lower side of the mounting frame 202, a processing tool 205 is installed on the lower end face of the rotating shaft 204, a placing table 3 is fixedly connected with the inner bottom end of the U-shaped processing table 1, two dust collecting boxes 4 are fixedly connected with the inner bottom end of the U-shaped processing table 1, the two dust collecting boxes 4 are respectively positioned on the left side and the right side of the placing table 3, the upper end faces of the two dust collecting boxes 4 are both communicated with a dust inlet pipe 401, dust suction fans 402 are installed on the outer side walls of the two dust inlet pipes 401, and dust suction heads 403 are installed at the opposite ends of the two dust inlet pipes 401.

In this embodiment: the model number of the dust suction fan 402 is: FLJ, the model number of cylinder 2 is: SD50, motor 203 model: YL, add man-hour, place the platform 3 upper end of placing with the engine part of treating processing, open cylinder 2 after that, connecting rod 201 drives processing tool 205 and removes corresponding position after, open motor 203, pivot 204 is rotatory to be driven processing tool 205 and is processed engine part, produce dust and piece easily in the course of working, the staff inhales for a long time and harms healthy easily, and then open two dust absorption fans 402 in the processing, the dust and the piece that processing produced enter into dust inlet pipe 401 through dust absorption head 403, carry to the case 4 that gathers dust next in, thereby reached and conveniently removed and collect the effect of processing the dust and the piece absorption that produce to processing in the engine part course of working, and conveniently make this processing equipment keep clean, avoid the staff to inhale the dust that processing produced for a long time and harm healthy problem.

As a technical optimization scheme, two risers 301 of the inside bottom fixedly connected with of U type processing platform 1, two risers 301 one end that carry on the back mutually respectively with two one end fixed connection relative of dust collecting box 4, automatically controlled telescopic link 302 is all installed to two relative one ends of riser 301, arc clamp splice 303 is all installed to two relative one ends of automatically controlled telescopic link 302, the lower terminal surface of two arc clamp splices 303 all with the up end parallel and level of placing platform 3.

In this embodiment: after an engine component to be processed is placed at the upper end of the placing table 3, the two electric control telescopic rods 302 are opened to drive the two arc-shaped clamping blocks 303 to clamp and fix the engine component at the upper end of the placing table 3, so that the effect of conveniently fixing the upper end of the placing table 3 on the engine component during processing of the engine component is achieved, and the problem of processing failure caused by displacement of the engine component in the processing process is avoided.

As a technical optimization scheme of the utility model, two dust collection box 4's preceding terminal surface all can be dismantled and be connected with and take out box 404, and handle 405 is all installed to two preceding terminal surfaces of taking out box 404.

In this embodiment: when processing the processing dust and the piece of collecting, hold handle 405, will take out box 404 and take out from dust collection box 4 the place ahead, handle the dust and the piece of taking out the collection in the box 404 to reach the effect that conveniently handles dust and the piece of taking out the collection in the box 404.

As a technical optimization scheme of the utility model, the equal fixedly connected with rubber pad 304 of inside wall of two arc clamp splices 303.

In this embodiment: when the two arc-shaped clamping blocks 303 clamp and fix the engine component to be processed, the rubber pads 304 avoid the problem that the outer wall of the engine component to be processed is damaged by the two arc-shaped clamping blocks 303.

As a technical optimization scheme of the utility model, place the up end fixedly connected with antiskid line 305 of platform 3.

In this embodiment: when the engine component to be processed is placed at the upper end of the placing table 3, the friction coefficient between the engine component to be processed and the placing table 3 is increased through the anti-skidding lines 305, and the problem that the engine component to be processed is easy to slide when placed at the upper end of the placing table 3 is avoided.

As a technical optimization scheme of the utility model, four evenly distributed's sucking disc stabilizer blade 101 are installed to the lower terminal surface of U type processing platform 1.

In this embodiment: the four sucker feet 101 improve the stability of the device when placed on the ground.

As a technical optimization scheme of the utility model, control panel 5 is installed to the preceding terminal surface of U type processing platform 1.

In this embodiment: when the equipment is processed, the operation and the closing of the equipment are conveniently controlled through the control panel 5.

The utility model discloses a theory of operation and use flow: during processing, an engine component to be processed is placed at the upper end of the placing table 3, after the engine component to be processed is placed at the upper end of the placing table 3, the two electric control telescopic rods 302 are opened to drive the two arc-shaped clamping blocks 303 to clamp and fix the engine component to the upper end of the placing table 3, then the cylinder 2 is opened, the connecting rod 201 drives the processing tool 205 to move to a corresponding position, the motor 203 is started, the rotating shaft 204 rotates to drive the processing tool 205 to process the engine component, dust and debris are easily generated during processing, workers easily damage the health after inhaling for a long time, then the two dust suction fans 402 are started during processing, the dust and debris generated during processing enter the dust inlet pipe 401 through the dust suction head 403 and are conveyed into the dust collection box 4, when the collected processing dust and debris are processed, the handle 405 is held by hands, the suction box 404 is drawn out from the front of the dust collection box 4, dust and debris collected within the drawer 404 is disposed of.

The above description is only exemplary of the present invention and should not be construed as limiting the present invention, and any modifications, equivalents and improvements made within the spirit and principles of the present invention are intended to be included within the scope of the present invention.

Claims

1. An aeroengine part processing equipment, includes U type processing platform (1), its characterized in that: the upper end face of the U-shaped processing table (1) is provided with an air cylinder (2), the output end of the air cylinder (2) is detachably connected with a connecting rod (201), the lower end of the connecting rod (201) penetrates through the U-shaped processing table (1) and extends into the U-shaped processing table (1), the lower end face of the connecting rod (201) is provided with an installation frame (202), the bottom end of the interior of the installation frame (202) is provided with a motor (203), the output end of the motor (203) is detachably connected with a rotating shaft (204), the lower end of the rotating shaft (204) penetrates through the installation frame (202) and extends to the lower part of the installation frame (202), the lower end face of the rotating shaft (204) is provided with a processing tool (205), the bottom end fixing connection of the interior of the U-shaped processing table (1) is provided with a placing table (3), and the bottom fixing connection of the interior of the U-shaped processing table (1) is provided with two dust collecting boxes (4), two dust collection box (4) are located the left and right sides of placing platform (3) respectively, two the up end of dust collection box (4) all communicates into dirt pipe (401), two dust absorption fan (402) are all installed to the lateral wall of entering dirt pipe (401), two dust absorption head (403) are all installed to the relative one end of entering dirt pipe (401).

2. An aircraft engine component machining apparatus according to claim 1, wherein: two risers (301) of inside bottom fixedly connected with of U type processing platform (1), two riser (301) one end that mutually backs on the back respectively with two one end fixed connection relative in dust collection box (4), two electric control telescopic link (302), two are all installed to the one end relative in riser (301) arc clamp splice (303), two are all installed to the one end relative in electric control telescopic link (302) the lower terminal surface of arc clamp splice (303) all with place the up end parallel and level of platform (3).

3. An aircraft engine component machining apparatus according to claim 1, wherein: the front end faces of the two dust collection boxes (4) can be detachably connected with a drawing box (404), and the front end faces of the two drawing boxes (404) are respectively provided with a handle (405).

4. An aircraft engine component machining apparatus according to claim 2, wherein: the inner side walls of the two arc-shaped clamping blocks (303) are fixedly connected with rubber pads (304).

5. An aircraft engine component machining apparatus according to claim 1, wherein: the upper end face of the placing table (3) is fixedly connected with anti-skid grains (305).

6. An aircraft engine component machining apparatus according to claim 1, wherein: four sucking disc support legs (101) which are uniformly distributed are arranged on the lower end face of the U-shaped processing table (1).

7. An aircraft engine component machining apparatus according to claim 1, wherein: and a control panel (5) is arranged on the front end face of the U-shaped processing table (1).